A novel airfoil circulation augment flow control method using co-flow jet

2nd AIAA Flow Control Conference

Volumn , Issue , 2004, Pages

  Zha, Ge Cheng ^a   Paxton, Craig ^a  

^a University of Miami College of Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; COMPUTATIONAL FLUID DYNAMICS; DRAG; EFFICIENCY; FLOW CONTROL; LIFT; MASS TRANSFER; PROPULSION;

AERO-DYNAMIC PERFORMANCE; AERODYNAMIC EFFICIENCY; CIRCULATION CONTROL; FLOW CONTROL METHODS; HIGH ANGLE OF ATTACK; NEGATIVE PRESSURES; SUBSONIC AIRCRAFT; SUBSONIC AIRFOILS;

JET AIRCRAFT;

EID: 85086491446     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-2208     Document Type: Conference Paper

References (19)

1. M. Gad-el Hak, "Flow Control: The Future, Journal of Aircraft, vol. 38, pp. 402-418, 2001.
2. M. Gad-el Hak, Flow Control, Passive, Active, and Reactive Flow Management. Cambridge University Press, 2000.
3. V. Modi, M. Fernando, and T. Yokomizo, "Drag Reduction of Bluff Bodies Through Moving Surface Boundary Layer Control." AIAA Paper No. 90-0298, 1990.
4. D. Cichy, J. Harris, and J. MacKay, "Flight Tests of a Rotating Cylinder Flap on a North American Rockwell YOV-10A Aircraft." NASA CR-2135, 1972.
5. L. C. Bradley, "An Experimental Investigation of A Sting-Mounted Finite Circulation Control Wing." M.S. Thesis, Air Force Institute of Technology, 1995.
6. N. Wood, L. Robert, and Z. Celik, "Control of Asymmetric Vortical Flows over Delta Wings at High Angle of Attack," Journal of Aircraft, vol. 27, pp. 429-435, 1990.
7. N. Wood and L. Robert, "Control of Vortical Lift on Delta Wings by Tangential Leading-Edge Blowing," Journal of Aircraft, vol. 25, pp. 236-243, 1988.
8. N. Wood and J. Nielsen, "Circulation Control Airfoils-Past, Present, Future." AIAA Paper 85-0204, 1985.
9. R. J. Englar, L. A. Trobaugh, and R. Hemmersly, "STOL Potential of the Circulation Control Wing for High-Performance Aircraft," Journal of Aircraft, vol. 14, pp. 175-181, 1978.
10. R. J. Englar, "Circulation Control for High Lift and Drag Generation on STOL Aircraft," Journal of Aircraft, vol. 12, pp. 457-463, 1975.
11. A. Smith, "High-Lift Aerodynamics," Journal of Aircraft, vol. 12, pp. 501-530, 1975.
12. J. Lin, S. Robinson, R. McGhee, and W. Valarezo, "Separation Control on High Reynolds Number Multi-Element Airfoils." AIAA Paper 92-2636, 1992.
13. K. McManus and J. Magill, "Airfoil Performance Enhancement Using Pulsed Jet Separation Control." AIAA Paper 97-1971, 1997.
14. K. McManus and J. Magill, "Separation Control in Incompressible and Compressible Flows Using Pulsed Jets." AIAA Paper 96-1948, 1996.
15. H. Johari and K. McManus, "Visulation of Pulsed Vortex Generator Jets for Active Control of Boundary Layer Separation." AIAA Paper 97-2021, 1997.
16. G.-C. Zha, (team members: David Car, and W. Copenhaver), "Super Diffusion Cascades Using Co-Flow Jet Flow Control." National Research Council Summer Faculty Final Report, Aug. 23, 2002.
17. D. Car, N. J. Kuprowicz, J. Estevadeordal, G.-C. Zha, and W. Copenhaver, "Stator Diffusion Enhancement Using A Re-circulating Co-flowing steady Jet." ASME GT-2004-53086, ASME TURBO EXPO 2004, June 14-17, 2004.
18. Y. Liu, L. N. Sankar, R. J. Englar, K. K. Ahuja, and R. Gaeta, "Computational Evaluation of the Steady and Pulsed Jet Effects on the Performance of a Circulation Control Wing Section." AIAA Paper 2004-0056, 42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada 5 - 8 Jan 2004.
19. J. Anderson J.D., Introduction to Flight, 4th edition. McGraw-Hill Higher Education, 2000.